Electrostatic air/oil separator for aircraft engine

B - Operations – Transporting – 01 – D

Patent

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Details

B01D 35/06 (2006.01) B01D 35/02 (2006.01) B01D 45/04 (2006.01) B01D 45/06 (2006.01) B03C 3/00 (2006.01) B64D 13/02 (2006.01) F01D 25/18 (2006.01) F01D 25/20 (2006.01) F01M 11/08 (2006.01)

Patent

CA 2663656

An air/oil separator (10 or 40) for use in a gas turbine engine comprises a labyrinth path (14 or 44) having an air/oil inlet (16 or 46), air outlet (18 or 48) and oil outlet (20 or 50), means (22, 24, 30 or 52, 54, 60) or creating an electrical field within the labyrinth path (14 or 44) and means (34 or 64) for creating a suction action at the oil outlet (20 or 50) to draw liquid oil from the labyrinth path (14 or 44) and for delivering the liquid oil under pressure to a pressurized source of oil in the engine.

L'invention concerne un séparateur air/huile (10 ou 40) destiné à être utilisé dans un moteur à turbine à gaz, qui comprend un trajet de labyrinthe (14 ou 44) ayant une entrée d'air/huile (16 ou 46), une sortie d'air (18 ou 48) et une sortie d'huile (20 ou 50), un moyen (22, 24, 30 ou 52, 54, 60) pour créer un champ électrique dans le trajet de labyrinthe (14 ou 44) et un moyen (34 ou 64) pour créer une action d'aspiration à la sortie d'huile (20 ou 50) pour extraire l'huile liquide du trajet de labyrinthe (14 ou 44) et pour distribuer l'huile liquide sous pression à une source pressurisée d'huile dans le moteur.

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